Modeling of an unmanned aerial vehicle (UAV) body for the needs of numerical aerodynamic investigations, strength analysis and examinations of free vibrations

被引：1
|
作者：
Kachel, Stanislaw [1 ]
Kozakiewicz, Adam [1 ]
机构：
[1] Military University of Technology, Kaliskiego g. 2, Warsaw,00-908, Poland
来源：
Solid State Phenomena | 2015年 / 220-221卷
关键词：
Aerodynamic modeling - Aircraft engineering - Free vibration - Master model - Panel model - Strength analysis - Virtual objects;
D O I：
10.4028/www.scientific.net/SSP.220-221.802
中图分类号：
学科分类号：
摘要：
19
引用
收藏
页码：802 / 807
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